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4. Quality Control of Composition, Microstructure and properties of refractories
[object Object],[object Object],[object Object],4.3  Study of their microstructure and microchemistry by  polarizing microscope (PM), scanning electron microscope (SEM) and electron-probe micro-analyzer (EPMA).
[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
[object Object],[object Object],[object Object],X  100, Where: l o  is the sample original length, l t  is the sample length after firing at a temperature t.
[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
[object Object]
[object Object],[object Object],True density =   (g/cm  ) Where : W 1   Weight of dry pyknometer W 2   Weight of pyknometer + fine sample,   W 3   Weight of pyknometer + fine sample +  liquid, W 4   Weight of pyknometer + liquid
[object Object],[object Object],True porosity =   x 100
[object Object],[object Object],[object Object]
[object Object],[object Object],[object Object],CCS or HCS  =   =  Rate of loading: -  2.0 kg/cm 2 / sec …. For dense Refractories , - 0.5 kg / cm 2  / sec ….  For lightweight refractories
. Cold- and hot- modulus of rupture, (CMOR and HMOR, kg/cm2, N/mm2 (MPa):  CMOR or HMOR are the capability of a rectangular bar sample to resist breaking by bending stress at room temperature or at high temperatures, respectively. They are calculated according the following equation: CMOR or HMOR. =  x  ,  [kg/cm 2 , N/mm 2  (MPa)],  Where: F  = Stress at which the sample is broken, L  = Sample length, W  = Sample width, R  =  Sample thickness   Rate of loading: - 1.5 kg / cm 2  / sec … For dense Refractories, - 0.5 kg / cm 2  / sec … For lightweight Refractories.
[object Object],[object Object],[object Object]
[object Object],[object Object],[object Object]
[object Object],[object Object],[object Object],Percentage of thermal expansion at t (oC) =  x 100  Coefficient of thermal expansion. at t (oC) =  Where:  L o   = original sample length at ambient temperature, L t   = sample length at the testing temperature, t, t o   = ambient temperature, t  =  testing temperature. ( o C -1 )
Figure 1: Reversible Linear Thermal Expansion of Some Refractories
[object Object],[object Object],[object Object]
[object Object],[object Object],[object Object]
[object Object],[object Object],[object Object],[object Object]
[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
[object Object],[object Object],K s  = thermal conductivity of the test sample (S), K K c = thermal conductivity of the calibrated sample, t 1  = temperature of the test sample hot face, t 2  = temperature of the test sample cold face and the calibrated  sample hot face,  t 3  = temperature of the calibrated sample cold face.
Figure 2: Thermal Conductivity Curves of Some Refractories
[object Object],[object Object],[object Object]
[object Object],[object Object]
[object Object],[object Object],[object Object]
[object Object],[object Object],[object Object],[object Object]
[object Object],[object Object],[object Object]
[object Object],[object Object],[object Object]
[object Object],[object Object],[object Object]
Figure 3: RUL Curves of Some Refractories
[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
[object Object],[object Object],[object Object]
Figure 4: EPMA-Line Scans Showing the Changes Occurred in the Chemical & Phase Composition and Densification Parameters of a Magnesia-Chrome Lining / Cement-Clinker Interface in the Clinkering Zone.
Specific Gravity & Prosity using Pycnometer
Specific Gravity using Pycnometer   W 1  (weight of Pycnometer ) W 2  (weight of Pycnometer + Sample ) W 4  (wt of Pycnometer+ Sample+ water ) W 3  (wt of Pycnometer+ Sample+kerosene )
Apparent Porosity D  (Dry weight of specimen ) S  (Suspended weight ) W  (Saturated Weight ) True porosity =  = [( ρ  –  B  ) /  ρ  ]100 Apparent Porosity
Sample Calculation ,[object Object],[object Object]
Solved example for : Density – and Porosity- calculations
Silicon carbide particles are compacted and fired at a high temperature to produce a strong ceramic shape. The specific gravity of SiC is 3.2 g/cm 3 .  The ceramic shape subsequently is weighed when dry (360 g), after soaking in water (385 g), and while suspended in water (224 g). Calculate the apparent porosity, the true porosity, and the fraction of the pore volume that is closed. Example 14.4 SOLUTION
Example 14.4 SOLUTION (Continued) The closed-pore percentage is the true porosity minus the apparent porosity, or 30 - 15.5 = 14.5%. Thus:
 

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The technological properties of refractory

  • 1. 4. Quality Control of Composition, Microstructure and properties of refractories
  • 2.
  • 3.
  • 4.
  • 5.
  • 6.
  • 7.
  • 8.
  • 9.
  • 10.
  • 11.
  • 12. . Cold- and hot- modulus of rupture, (CMOR and HMOR, kg/cm2, N/mm2 (MPa): CMOR or HMOR are the capability of a rectangular bar sample to resist breaking by bending stress at room temperature or at high temperatures, respectively. They are calculated according the following equation: CMOR or HMOR. = x , [kg/cm 2 , N/mm 2 (MPa)], Where: F = Stress at which the sample is broken, L = Sample length, W = Sample width, R = Sample thickness Rate of loading: - 1.5 kg / cm 2 / sec … For dense Refractories, - 0.5 kg / cm 2 / sec … For lightweight Refractories.
  • 13.
  • 14.
  • 15.
  • 16. Figure 1: Reversible Linear Thermal Expansion of Some Refractories
  • 17.
  • 18.
  • 19.
  • 20.
  • 21.
  • 22. Figure 2: Thermal Conductivity Curves of Some Refractories
  • 23.
  • 24.
  • 25.
  • 26.
  • 27.
  • 28.
  • 29.
  • 30. Figure 3: RUL Curves of Some Refractories
  • 31.
  • 32.
  • 33.
  • 34. Figure 4: EPMA-Line Scans Showing the Changes Occurred in the Chemical & Phase Composition and Densification Parameters of a Magnesia-Chrome Lining / Cement-Clinker Interface in the Clinkering Zone.
  • 35. Specific Gravity & Prosity using Pycnometer
  • 36. Specific Gravity using Pycnometer W 1 (weight of Pycnometer ) W 2 (weight of Pycnometer + Sample ) W 4 (wt of Pycnometer+ Sample+ water ) W 3 (wt of Pycnometer+ Sample+kerosene )
  • 37. Apparent Porosity D (Dry weight of specimen ) S (Suspended weight ) W (Saturated Weight ) True porosity = = [( ρ – B ) / ρ ]100 Apparent Porosity
  • 38.
  • 39. Solved example for : Density – and Porosity- calculations
  • 40. Silicon carbide particles are compacted and fired at a high temperature to produce a strong ceramic shape. The specific gravity of SiC is 3.2 g/cm 3 . The ceramic shape subsequently is weighed when dry (360 g), after soaking in water (385 g), and while suspended in water (224 g). Calculate the apparent porosity, the true porosity, and the fraction of the pore volume that is closed. Example 14.4 SOLUTION
  • 41. Example 14.4 SOLUTION (Continued) The closed-pore percentage is the true porosity minus the apparent porosity, or 30 - 15.5 = 14.5%. Thus:
  • 42.